Active Flow Control of Delta Wing Leading-Edge Vortices
A. Kölzsch
Abstract
A. Kölzsch
Abstract
This work presents a comprehensive experimental investigation of two active flow control methods on a generic delta wing configuration. Both actuation techniques namely pulsed blowing near the leading edge and oscillating leading-edge flaps, allow for frequency-dependent forcing of the leading-edge vortex system and its inherent instabilities. A parameter study and the systematic analysis of the results show the aerodynamic potential of each method.
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This work presents a comprehensive experimental investigation of two active flow control methods on a generic delta wing configuration. Both actuation techniques namely pulsed blowing near the leading edge and oscillating leading-edge flaps, allow for frequency-dependent forcing of the leading-edge vortex system and its inherent instabilities. A parameter study and the systematic analysis of the results show the aerodynamic potential of each method.
Key concepts: Delta wing, Leading edge, Wing, Vortex, Aerodynamics, Enhanced Data Rates for GSM Evolution, Flow (mathematics), Forcing (mathematics)